ekf2: add terrain state

This commit is contained in:
bresch
2024-06-26 11:05:38 +02:00
committed by Silvan Fuhrer
parent 09f066a73a
commit 68980b59e2
53 changed files with 1936 additions and 1930 deletions
+4 -6
View File
@@ -107,7 +107,7 @@ enum MagFuseType : uint8_t {
#endif // CONFIG_EKF2_MAGNETOMETER
#if defined(CONFIG_EKF2_TERRAIN)
enum TerrainFusionMask : uint8_t {
enum class TerrainFusionMask : uint8_t {
TerrainFuseRangeFinder = (1 << 0),
TerrainFuseOpticalFlow = (1 << 1)
};
@@ -382,8 +382,8 @@ struct parameters {
#endif // CONFIG_EKF2_SIDESLIP
#if defined(CONFIG_EKF2_TERRAIN)
int32_t terrain_fusion_mode{TerrainFusionMask::TerrainFuseRangeFinder |
TerrainFusionMask::TerrainFuseOpticalFlow}; ///< aiding source(s) selection bitmask for the terrain estimator
int32_t terrain_fusion_mode{static_cast<int32_t>(TerrainFusionMask::TerrainFuseRangeFinder)
| static_cast<int32_t>(TerrainFusionMask::TerrainFuseOpticalFlow)}; ///< aiding source(s) selection bitmask for the terrain estimation
float terrain_p_noise{5.0f}; ///< process noise for terrain offset (m/sec)
float terrain_gradient{0.5f}; ///< gradient of terrain used to estimate process noise due to changing position (m/m)
@@ -401,10 +401,8 @@ struct parameters {
float range_delay_ms{5.0f}; ///< range finder measurement delay relative to the IMU (mSec)
float range_noise{0.1f}; ///< observation noise for range finder measurements (m)
float range_innov_gate{5.0f}; ///< range finder fusion innovation consistency gate size (STD)
float rng_hgt_bias_nsd{0.13f}; ///< process noise for range height bias estimation (m/s/sqrt(Hz))
float rng_sens_pitch{0.0f}; ///< Pitch offset of the range sensor (rad). Sensor points out along Z axis when offset is zero. Positive rotation is RH about Y axis.
float range_noise_scaler{0.0f}; ///< scaling from range measurement to noise (m/m)
const float vehicle_variance_scaler{0.0f}; ///< gain applied to vehicle height variance used in calculation of height above ground observation variance
float max_hagl_for_range_aid{5.0f}; ///< maximum height above ground for which we allow to use the range finder as height source (if rng_control == 1)
float max_vel_for_range_aid{1.0f}; ///< maximum ground velocity for which we allow to use the range finder as height source (if rng_control == 1)
float range_aid_innov_gate{1.0f}; ///< gate size used for innovation consistency checks for range aid fusion
@@ -521,7 +519,7 @@ union innovation_fault_status_u {
bool reject_yaw : 1; ///< 7 - true if the yaw observation has been rejected
bool reject_airspeed : 1; ///< 8 - true if the airspeed observation has been rejected
bool reject_sideslip : 1; ///< 9 - true if the synthetic sideslip observation has been rejected
bool reject_hagl : 1; ///< 10 - true if the height above ground observation has been rejected
bool reject_hagl : 1; ///< 10 - unused
bool reject_optflow_X : 1; ///< 11 - true if the X optical flow observation has been rejected
bool reject_optflow_Y : 1; ///< 12 - true if the Y optical flow observation has been rejected
} flags;